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Calculation of three-dimensional turbulent boundary layers

Published online by Cambridge University Press:  29 March 2006

P. Bradshaw
Affiliation:
National Physical Laboratory, Teddington
Department of Aeronautics, Imperial College, London S.W. 7

Abstract

The two-dimensional prediction method of Bradshaw, Ferriss & Atwell (1967), which was based on the empirical conversion of the turbulent energy equation into a ‘transport’ equation for shear stress, is extended to three-dimensional flows satisfying the boundary-layer approximation (which excludes flows near bluff obstacles or streamwise corners). Predictions, using exactly the same empirical data as in two-dimensional flow, agree to within the likely experimental error with a variety of experiments on ‘infinite’ swept wings.

Type
Research Article
Copyright
© 1971 Cambridge University Press

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References

Angell, J. K., Pack, D. H. & Dickson, C. R. 1968 J. Atmos. Sci. 25, 707.
Ashkenas, H. 1958 N.A.C.A. Tech. Note no. 4140.
Ashkenas, H. & Riddell, F. R. 1955 N.A.C.A. Tech. Note no. 3383.
Bradshaw, P. 1967 J. Fluid Mech. 30, 241.
Bradshaw, P. 1968 Nat. Phys. Lab. Aero. Rep. no. 1232.
Bradshaw, P. 1969a Nat. Phys. Lab. Aero. Rep. no. 1288.
Bradshaw, P. 1969b J. Fluid Mech. 35, 387.
Bradshaw, P. 1969c J. Fluid Mech. 36, 177.
Bradshaw, P. 1970 Imperial College Aero. Rep. no. 70–06.
Bradshaw, P. & Ferriss, D. H. 1965 Nat. Phys. Lab. Aero. Rep. no. 1145 (and Addendum 1968).
Bradshaw, P. & Ferriss, D. H. 1971 J. Fluid Mech. 46, 83.
Bradshaw, P., Ferriss, D. H. & Atwell, N. P. 1967 J. Fluid Mech. 28, 593.
Bradshaw, P. & Terrell, M. G. 1969 Nat. Phys. Lab. Aero. Rep. no. 1305.
Coles, D. E. 1962 Rand Corp. Rep. no. R-403-PR and Aero. Res. Counc. paper no. 24497 (1963).
Crow, S. C. 1968 J. Fluid Mech. 33, 1.
Cumpsty, N. A. & Head, M. R. 1967a Aero. Quart. 18, 55.
Cumpsty, N. A. & Head, M. R. 1967b Aero. Quart. 18, 150.
Cumpsty, N. A. & Head, M. R. 1970 Aero. Quart. 21, 121.
Donaldson, C. Dup., Sullivan, R. & Rosenbaum, H. 1970 A.I.A.A. paper no. 70–55.
Eichelbrenner, E. A. & Oudart, A. 1955 O.N.E.R.A., Paris, pub. no. 76.
Etheridge, D. 1970 Ph.D. Thesis, Queen Mary Coll., London University.
Ferriss, D. H. 1969 Nat. Phys. Lab. Aero. Rep. no. 1295.
Horton, H. P. 1969 Hawker Siddeley Aviation (Hatfield) Research Rep. 1094/HPH.
Johnston, J. P. 1970 J. Fluid Mech. 42, 823.
Keffer, J. H. 1965 J. Fluid Mech. 22, 135.
Keffer, J. H. 1967 J. Fluid Mech. 28, 183.
Kline, S. J., Morkovin, M. V., Sovran, G. & Cockrell, D. J. 1969 Proceedings, Computation of Turbulent Boundary Layers—1968 AFOSR—IFP—Stanford Conference, Thermosciences Divn., Stanford University.
Kovasznay, L. S. G. & Hall, M. G. 1967 A.I.A.A. J. 5, 2065.
Kuettner, J. P. 1968 Aero. Revue, p. 52 and p. 109.
Martin, D. W. & Ferriss, D. H. 1969 Nat. Phys. Lab. Maths. Rep. no. 74.
Nash, J. F. 1969 J. Fluid Mech. 37, 625.
Patel, V. C. & Head, M. R. 1968 J. Fluid Mech. 34, 371.
Townsend, A. A. 1956 The Structure of Turbulent Shear Flow. Cambridge University Press.
Wesseling, P. 1969 N.L.R. (Amsterdam) Rep. no. AT-69–01.
Winter, K. G., Rotta, J. C. & Smith, K. G. 1968 R.A.E. Tech. Rep. no. 68215.